Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4:
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Washington, DC
National Aeronautics and Space Administration
1960
|
| Schriftenreihe: | NASA technical note
D-7 |
| Schlagworte: | |
| Beschreibung: | 42 S. Ill., graph. Darst. 27 cm |
Internformat
MARC
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| 049 | |a DE-210 | ||
| 100 | 1 | |a Gillis, Clarence L. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4 |c by Clarence L. Gillis and A. James Vitale |
| 264 | 1 | |a Washington, DC |b National Aeronautics and Space Administration |c 1960 | |
| 300 | |a 42 S. |b Ill., graph. Darst. |c 27 cm | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 1 | |a NASA technical note |v D-7 | |
| 650 | 0 | 7 | |a Auftrieb |0 (DE-588)4137274-8 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Modellflugzeug |0 (DE-588)4170295-5 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Raketentriebwerk |0 (DE-588)4176905-3 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Aerodynamik |0 (DE-588)4000589-6 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Flugzeug |0 (DE-588)4017672-1 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Tragflügelaerodynamik |0 (DE-588)4185832-3 |2 gnd |9 rswk-swf |
| 689 | 0 | 0 | |a Aerodynamik |0 (DE-588)4000589-6 |D s |
| 689 | 0 | 1 | |a Auftrieb |0 (DE-588)4137274-8 |D s |
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| 689 | 0 | 3 | |a Raketentriebwerk |0 (DE-588)4176905-3 |D s |
| 689 | 0 | |5 DE-604 | |
| 689 | 1 | 0 | |a Flugzeug |0 (DE-588)4017672-1 |D s |
| 689 | 1 | 1 | |a Raketentriebwerk |0 (DE-588)4176905-3 |D s |
| 689 | 1 | 2 | |a Tragflügelaerodynamik |0 (DE-588)4185832-3 |D s |
| 689 | 1 | |5 DE-604 | |
| 689 | 2 | 0 | |a Aerodynamik |0 (DE-588)4000589-6 |D s |
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| 689 | 2 | 2 | |a Modellflugzeug |0 (DE-588)4170295-5 |D s |
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| 689 | 3 | 2 | |a Tragflügelaerodynamik |0 (DE-588)4185832-3 |D s |
| 689 | 3 | |5 DE-604 | |
| 700 | 1 | |a Vitale, A. James |e Verfasser |4 aut | |
| 830 | 0 | |a NASA technical note |v D-7 |w (DE-604)BV021854105 |9 7 | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-017709741 | ||
Datensatz im Suchindex
| _version_ | 1804139342812151808 |
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| any_adam_object | |
| author | Gillis, Clarence L. Vitale, A. James |
| author_facet | Gillis, Clarence L. Vitale, A. James |
| author_role | aut aut |
| author_sort | Gillis, Clarence L. |
| author_variant | c l g cl clg a j v aj ajv |
| building | Verbundindex |
| bvnumber | BV035655229 |
| ctrlnum | (OCoLC)249942630 (DE-599)GBV378228552 |
| format | Book |
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| id | DE-604.BV035655229 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T21:42:34Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-017709741 |
| oclc_num | 249942630 |
| open_access_boolean | |
| owner | DE-210 |
| owner_facet | DE-210 |
| physical | 42 S. Ill., graph. Darst. 27 cm |
| publishDate | 1960 |
| publishDateSearch | 1960 |
| publishDateSort | 1960 |
| publisher | National Aeronautics and Space Administration |
| record_format | marc |
| series | NASA technical note |
| series2 | NASA technical note |
| spelling | Gillis, Clarence L. Verfasser aut Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4 by Clarence L. Gillis and A. James Vitale Washington, DC National Aeronautics and Space Administration 1960 42 S. Ill., graph. Darst. 27 cm txt rdacontent n rdamedia nc rdacarrier NASA technical note D-7 Auftrieb (DE-588)4137274-8 gnd rswk-swf Modellflugzeug (DE-588)4170295-5 gnd rswk-swf Raketentriebwerk (DE-588)4176905-3 gnd rswk-swf Aerodynamik (DE-588)4000589-6 gnd rswk-swf Flugzeug (DE-588)4017672-1 gnd rswk-swf Tragflügelaerodynamik (DE-588)4185832-3 gnd rswk-swf Aerodynamik (DE-588)4000589-6 s Auftrieb (DE-588)4137274-8 s Flugzeug (DE-588)4017672-1 s Raketentriebwerk (DE-588)4176905-3 s DE-604 Tragflügelaerodynamik (DE-588)4185832-3 s Modellflugzeug (DE-588)4170295-5 s Vitale, A. James Verfasser aut NASA technical note D-7 (DE-604)BV021854105 7 |
| spellingShingle | Gillis, Clarence L. Vitale, A. James Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4 NASA technical note Auftrieb (DE-588)4137274-8 gnd Modellflugzeug (DE-588)4170295-5 gnd Raketentriebwerk (DE-588)4176905-3 gnd Aerodynamik (DE-588)4000589-6 gnd Flugzeug (DE-588)4017672-1 gnd Tragflügelaerodynamik (DE-588)4185832-3 gnd |
| subject_GND | (DE-588)4137274-8 (DE-588)4170295-5 (DE-588)4176905-3 (DE-588)4000589-6 (DE-588)4017672-1 (DE-588)4185832-3 |
| title | Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4 |
| title_auth | Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4 |
| title_exact_search | Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4 |
| title_full | Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4 by Clarence L. Gillis and A. James Vitale |
| title_fullStr | Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4 by Clarence L. Gillis and A. James Vitale |
| title_full_unstemmed | Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4 by Clarence L. Gillis and A. James Vitale |
| title_short | Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4 |
| title_sort | wing on and wing off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3 as obtained from rocket propelled models at mach numbers from 0 8 to 1 4 |
| topic | Auftrieb (DE-588)4137274-8 gnd Modellflugzeug (DE-588)4170295-5 gnd Raketentriebwerk (DE-588)4176905-3 gnd Aerodynamik (DE-588)4000589-6 gnd Flugzeug (DE-588)4017672-1 gnd Tragflügelaerodynamik (DE-588)4185832-3 gnd |
| topic_facet | Auftrieb Modellflugzeug Raketentriebwerk Aerodynamik Flugzeug Tragflügelaerodynamik |
| volume_link | (DE-604)BV021854105 |
| work_keys_str_mv | AT gillisclarencel wingonandwingofflongitudinalcharacteristicsofanairplaneconfigurationhavingathinunsweptwingofaspectratio3asobtainedfromrocketpropelledmodelsatmachnumbersfrom08to14 AT vitaleajames wingonandwingofflongitudinalcharacteristicsofanairplaneconfigurationhavingathinunsweptwingofaspectratio3asobtainedfromrocketpropelledmodelsatmachnumbersfrom08to14 |